Reinforced superplastic formed and diffusion bonded structures

Patent metadata

Field	Value
Publication number	US-11260952-B2
Application number	US-201916584377-A
Country	US
Kind code	B2
Filing date	Sep 26, 2019
Priority date	Sep 26, 2019
Publication date	Mar 1, 2022
Grant date	Mar 1, 2022

Abstract

An exterior panel is formed of superplastic materials, including an exterior skin of titanium to accommodate high thermal stresses imposed on hypersonic transport vehicles during hypersonic flight. The exterior skin is fixed to an underlying reinforcing skeletal structure consisting of a superplastic formable reinforcement (SFR) layer, for example a titanium, zirconium, and molybdenum (TZM) alloy, which supports the exterior skin whenever the latter may be heated to temperatures exceeding 1200 degrees Fahrenheit. The exterior panel includes a separate interior skin configured for attachment to a frame member such as a rib, stringer, or spar of the hypersonic transport vehicle. A multicellular core is sandwiched between the exterior and interior skins to impart tensile and compressive strength to the exterior panel. In one disclosed method, the core is superplastic formed and diffusion bonded to the exterior and interior skins.

First claim

What is claimed is:

1. An exterior panel for transport vehicle, the exterior panel comprising:
an exterior skin of a superplastic material configured for atmospheric exposure;
an interior skin of a superplastic material configured for attachment to a structural frame member of the transport vehicle;
a multicellular core sandwiched between the exterior skin and the interior skin, the multicellular core comprising at least a pair of core sheets of a superplastic material bonded together via intermittent seam welds arrayed in a predetermined patterned; continuously welded about the edges of the core sheets and
a superplastic formable reinforcement (SFR) layer underlying and secured to the exterior skin, the SFR layer configured to support the exterior skin when an atmospheric friction temperature of the exterior skin exceeds 1200 degrees Fahrenheit,
wherein the multicellular core is superplastic formed and diffusion bonded to the exterior skin and the interior skin.

2. The exterior panel of claim 1 , wherein all components except the SFR layer are formed of a titanium alloy.

3. The exterior panel of claim 1 , wherein the SFR layer is formed of a superplastic formable alloy consisting of titanium, zirconium, and molybdenum (TZM).

4. The exterior panel of claim 1 , wherein the SFR layer is formed of a ferrous-nickel-cobalt alloy.

5. The exterior panel of claim 1 , wherein the SFR layer comprises a skeletal structure underlying 20 to 80% of the exterior skin.

6. The exterior panel of claim 1 , wherein the SFR layer is 80 to 150 percent of a thickness of the exterior skin.

7. A transport vehicle having at least one exterior panel, the at least one exterior panel comprising:
an exterior skin of a superplastic material configured for atmospheric exposure;
an interior skin of a superplastic material configured for attachment to a structural frame member of the transport vehicle;
a multicellular core configured to impart tensile and compressive strength to the exterior panel, the multicellular core being sandwiched between the exterior skin and the interior skin, and the multicellular core comprising at least a pair of core sheets of a superplastic material bonded together via intermittent seam welds arrayed in a predetermined pattern; continuously welded about the edges of the core sheets and
an SFR layer that underlies, is secured to, and supports the exterior skin when an atmospheric temperature on the exterior skin exceeds 1200 degrees Fahrenheit;
wherein the multicellular core is superplastic formed and diffusion bonded to the exterior skin and the interior skin.

8. The transport vehicle of claim 7 , wherein the transport vehicle is a hypersonic vehicle having a plurality of exterior panels, and wherein each exterior panel is fusion welded to at least one other exterior panel.

9. The transport vehicle of claim 8 , wherein each SFR layer of each of the plurality of exterior panels includes an SFR layer, welded to the exterior skin to reinforce the exterior skin above temperatures of 1200 degrees Fahrenheit.

10. The transport vehicle of claim 7 , wherein the SFR layer is formed of a TZM material.

11. The transport vehicle of claim 7 , wherein the SFR layer is formed of a ferrous-nickel-cobalt alloy.

12. A method of manufacturing an exterior panel for a transport vehicle, the method comprising:
providing an exterior skin of a superplastic material configured for atmospheric exposure;
providing a SFR layer to be fixed adjacent the exterior skin, the SFR layer configured to support the exterior skin when an atmospheric friction temperature of the exterior skin exceeds 1200 degrees Fahrenheit;
providing an interior skin of a superplastic material configured for attachment to a structural frame member of the transport vehicle;
providing at least a pair of core sheets of a superplastic material for forming a multicellular core between the exterior skin and the interior skin; then
securing the SFR layer to the exterior skin;
bonding the pair of core sheets together via intermittent seam welds arrayed in a predetermined pattern, securing an expansion pipe to one edge of the core sheets, and the applying a continuous weld about the edges of the core sheets; and
installing the exterior skin and the interior skin with the core sheets into a pressure containment device, supplying an inert gas into the expansion pipe to superplastic form and diffusion bond the exterior skin, the interior skin and the core sheets, creating a multicellular core that is integrally bonded to the exterior skin and the interior skin.

13. The method of claim 12 , wherein the SFR layer is secured to the exterior skin by welding.

14. The method of claim 12 , wherein the SFR layer is formed of a TZM material.

15. The method of claim 12 , wherein the SFR layer is formed of a ferrous-nickel-cobalt alloy.

16. The method of claim 12 , wherein the SFR layer is 80 to 150 percent of a thickness of the exterior skin.

17. The method of claim 12 , wherein the SFR layer underlies 20 to 80 percent of the exterior skin.

18. The method of claim 12 , wherein the SFR layer comprises a skeletal structure underlying the exterior skin.

19. The exterior panel of claim 1 , wherein the SFR layer is secured to the exterior skin by welding.

20. The method of claim 12 , wherein all components except the SFR layer are formed of a titanium alloy.

Assignees

• Boeing Co

Inventors

• Vasel Corey

Classifications

• B29C65/00

  Joining {or sealing} of preformed parts {, e.g. welding of plastics materials}; Apparatus therefor {(general aspects of processes or apparatus for joining preformed parts B29C66/00; using porous material formed by internal pressure generated therein for joining preformed parts B29C44/1228, B29C44/326)} · CPC title

• B29C66/72525

  comprising honeycomb cores · CPC title

• B21D39/031

  Joining superposed plates by locally deforming without slitting or piercing · CPC title

• B64G1/58 Primary

  Thermal protection, e.g. heat shields · CPC title

• B29C65/006

  Diffusion joining (measures for intermixing the material of the joint interlayer B29C66/341) · CPC title